AD 93-04-03

final rule
Data completeness: 70%

Airworthiness Directives; General Dynamics Model 340, 440, and C-131B through C-131H (military) Series Airplanes

AD Number
93-04-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
92-NM-202-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Kelowna Flightcraft R & D Ltd. 340 Airworthiness Directives; General Dynamics Model 340, 440, and C-131B through C-131H (military) Series Airplanes
aircraft Kelowna Flightcraft R & D Ltd. 440 Airworthiness Directives; General Dynamics Model 340, 440, and C-131B through C-131H (military) Series Airplanes
aircraft Kelowna Flightcraft R & D Ltd. Military C-131B Airworthiness Directives; General Dynamics Model 340, 440, and C-131B through C-131H (military) Series Airplanes
aircraft Kelowna Flightcraft R & D Ltd. Military C-131D Airworthiness Directives; General Dynamics Model 340, 440, and C-131B through C-131H (military) Series Airplanes
aircraft Kelowna Flightcraft R & D Ltd. Military C-131E Airworthiness Directives; General Dynamics Model 340, 440, and C-131B through C-131H (military) Series Airplanes
aircraft Kelowna Flightcraft R & D Ltd. Military C-131F/R4Y-1 Airworthiness Directives; General Dynamics Model 340, 440, and C-131B through C-131H (military) Series Airplanes

Unsafe Condition

Failure of the stabilizer attach fittings, and potential subsequent loss of a horizontal or vertical stabilizer.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Within 12 months or 1,500 flight hours after the effective date, inspect horizontal and vertical stabilizer attach fittings per Service Bulletin 640(340D) S.B. No. 55-6. Perform hardness tests on taper pins and split sleeve bushings to ensure equivalent strength between 160-180 ksi. Replace discrepant parts with FAA-approved new parts. Ensure new parts meet hardness requirements before installation.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 12 months or 1,500 flight hours after the effective date of this AD, whichever occurs first

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

General Dynamics Model 340, 440, and C-131B through C-131H (military) series airplanes, all serial numbers, including those modified for turbo-propeller power.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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